CA2832493A1 - Ensemble de turbines a gaz et procede permettant de faire fonctionner celui-ci - Google Patents

Ensemble de turbines a gaz et procede permettant de faire fonctionner celui-ci Download PDF

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Publication number
CA2832493A1
CA2832493A1 CA2832493A CA2832493A CA2832493A1 CA 2832493 A1 CA2832493 A1 CA 2832493A1 CA 2832493 A CA2832493 A CA 2832493A CA 2832493 A CA2832493 A CA 2832493A CA 2832493 A1 CA2832493 A1 CA 2832493A1
Authority
CA
Canada
Prior art keywords
burner
gas turbine
turbine assembly
combustion
combustion chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA2832493A
Other languages
English (en)
Other versions
CA2832493C (fr
Inventor
Robert Marmilic
Jaan Hellat
Ewald Freitag
Adnan Eroglu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ansaldo Energia Switzerland AG
Original Assignee
Alstom Technology AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alstom Technology AG filed Critical Alstom Technology AG
Publication of CA2832493A1 publication Critical patent/CA2832493A1/fr
Application granted granted Critical
Publication of CA2832493C publication Critical patent/CA2832493C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/228Dividing fuel between various burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/346Feeding into different combustion zones for staged combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/70Application in combination with
    • F05D2220/72Application in combination with a steam turbine
    • F05D2220/722Application in combination with a steam turbine as part of an integrated gasification combined cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03341Sequential combustion chambers or burners
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/16Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/16Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
    • Y02E20/18Integrated gasification combined cycle [IGCC], e.g. combined with carbon capture and storage [CCS]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Combustion Of Fluid Fuel (AREA)
CA2832493A 2011-04-08 2012-04-05 Ensemble de turbines a gaz et procede permettant de faire fonctionner celui-ci Expired - Fee Related CA2832493C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH00636/11A CH704829A2 (de) 2011-04-08 2011-04-08 Gasturbogruppe und zugehöriges Betriebsverfahren.
CH636/11 2011-04-08
PCT/EP2012/056323 WO2012136787A1 (fr) 2011-04-08 2012-04-05 Ensemble de turbines à gaz et procédé permettant de faire fonctionner celui-ci

Publications (2)

Publication Number Publication Date
CA2832493A1 true CA2832493A1 (fr) 2012-10-11
CA2832493C CA2832493C (fr) 2017-05-30

Family

ID=46001168

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2832493A Expired - Fee Related CA2832493C (fr) 2011-04-08 2012-04-05 Ensemble de turbines a gaz et procede permettant de faire fonctionner celui-ci

Country Status (11)

Country Link
US (1) US10774740B2 (fr)
EP (1) EP2694878B1 (fr)
JP (1) JP5946519B2 (fr)
KR (1) KR101638333B1 (fr)
CN (1) CN103443542B (fr)
BR (1) BR112013025839A2 (fr)
CA (1) CA2832493C (fr)
CH (1) CH704829A2 (fr)
MX (1) MX2013010930A (fr)
RU (1) RU2563446C2 (fr)
WO (1) WO2012136787A1 (fr)

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US10330319B2 (en) 2012-10-24 2019-06-25 Ansaldo Energia Switzerland AG Sequential combustion with dilution gas mixer

Also Published As

Publication number Publication date
EP2694878B1 (fr) 2018-12-12
CN103443542A (zh) 2013-12-11
BR112013025839A2 (pt) 2016-12-20
JP5946519B2 (ja) 2016-07-06
RU2013149862A (ru) 2015-05-20
US10774740B2 (en) 2020-09-15
MX2013010930A (es) 2014-06-05
CA2832493C (fr) 2017-05-30
JP2014510256A (ja) 2014-04-24
CH704829A2 (de) 2012-11-15
CN103443542B (zh) 2016-10-26
US20140033728A1 (en) 2014-02-06
EP2694878A1 (fr) 2014-02-12
KR101638333B1 (ko) 2016-07-12
KR20140027237A (ko) 2014-03-06
RU2563446C2 (ru) 2015-09-20
WO2012136787A1 (fr) 2012-10-11

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